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Sliding mode control of a reusable l...

Hall, Charles E.

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Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation./
作者:	Hall, Charles E.
面頁冊數:	143 p.
附註:	Source: Masters Abstracts International, Volume: 43-03, page: 0899.
Contained By:	Masters Abstracts International43-03.
標題:	Engineering, Aerospace. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=1423592
ISBN:	0496112163

Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation.
Hall, Charles E.

Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation. - 143 p.

Source: Masters Abstracts International, Volume: 43-03, page: 0899.

Thesis (M.S.E.)--The University of Alabama in Huntsville, 2005.

In this work, a flight control system for a reusable launch vehicle during Terminal Area Energy Management (TAEM), approach and landing phases of flight is developed and then tested in a high fidelity, nonlinear six degree of freedom simulation. A new control algorithm based on multiple time scale Sliding Mode Control, driven by sliding mode disturbance observers using gain adaptation is designed. Comparisons with a classical, gain scheduled PID controller are made and considerable improvements in performance are shown. The developed Sliding Mode Control system has potential to improve vehicle safety and reliability through robustness to disturbances, and to decrease development and operational cost by reduced analysis time and improved launch availability.

ISBN: 0496112163Subjects--Topical Terms:

1018395
Engineering, Aerospace.

Sliding mode control of a reusable launch vehicle using sliding mode observers and gain adaptation.
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520 $a In this work, a flight control system for a reusable launch vehicle during Terminal Area Energy Management (TAEM), approach and landing phases of flight is developed and then tested in a high fidelity, nonlinear six degree of freedom simulation. A new control algorithm based on multiple time scale Sliding Mode Control, driven by sliding mode disturbance observers using gain adaptation is designed. Comparisons with a classical, gain scheduled PID controller are made and considerable improvements in performance are shown. The developed Sliding Mode Control system has potential to improve vehicle safety and reliability through robustness to disturbances, and to decrease development and operational cost by reduced analysis time and improved launch availability.
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